发明名称 Soft landing gear
摘要 A bogie type landing gear especially suitable for providing soft landing capabilities for short take-off and landing (STOL) aircraft wherein fore and aft wheels are mounted on opposite ends of a bogie which is pivotally attached to the lower end of a vertical shock strut. In one embodiment, a torque link pivotally connects the aft end of the bogie to the shock strut such that, under normal landing conditions, the front wheel will touch down first thereby reducing and directing the landing forces to minimize shock to the aircraft. The aft mounted torque links also act as a tension member during the initial landing stroke. In another embodiment, a damper acts as a tension stop for a soft landing arrangement as well as to dampen bogie motion over bumps with the torque links being separate.
申请公布号 US4359199(A) 申请公布日期 1982.11.16
申请号 US19790100321 申请日期 1979.12.05
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE AIR FORCE 发明人 KRAMER, LOUIS T.;BUTLER, FRANKLIN H.;CAMINO, ANTHONY V.
分类号 B64C25/34;(IPC1-7):B64C25/40 主分类号 B64C25/34
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